11.4 Air Conditioning & Cabin Pressurisation - 14Q Flashcards
Name the sources of pneumatic air supply for air-conditioning
Primary bleed air = Engines
Secondary bleed air = APU, pneumatic ground cart
What area’s of an engine is air tapped from for supplying pneumatics to air-conditioning
Bleed air from the engines normally supplies the air conditioning systems
What is the most economical pneumatic source on the ground?
External air conditioning sources are more economical
What is the purpose of an emergency ram air system?
The system can be used in flight to ventilate the cockpit and cabin if all packs fail
or
for smoke removal only
(If ram air is used in flight, pressure differential must be no greater than 1 psi)
When using a pneumatic ground car to supply the air-con packs, you must ensure what?
Ensure that the air conditioning pack sources (APU,engines) are not also suppling air.
Air conditioning packs and external air conditioning sources should not supply an aircraft simultaneously to prevent excessive cabin airflow and possible air conditioning duct damage.
What can feed the Pack 1 air conditioning system?
(Isolation valve closed)
Engine 1
APU
Pneumatic ground cart
What can feed air conditioning PACK 2 ?
(Isolation valve closed)
Engine 2 only
What can the ground conditioned air connector do?
Ground conditioned air connected can feed air directly into the cabin, bypasssing all pack systems
If the ram air pushbutton is actuated, the _______ open to discharge the cabin pressure and the _________ opens to allow a ram air flow through the cockpit and cabin
outflow valve
ram air door
The ram air pushbutton should not be actuated before the cabin/ambient differential pressure is below _______ to prevent a rapid decompression of the cabin
1 psi
(c)
(b)
(c) Evaporator
Evaporator takes the absorbs the heat from the aircraft cabin into the refrigerant which causes it to evaporate.
Condensor condenses the hot refrigerant gas coming from the compressor. This is where the heat in the refrigerant is given up to the outside ambient temperature
Evaporator absorbs heat from cabin, condensor absorbs heat from refrigerant
(c) The turbine
(b) The structural stength of the aircraft cabin
(b) Cabin is not pressurised
(b) the outflow valve must be closed
(a) To regulate the cabin pressure
What is the purpose of an air-conditioning system?
(3 variables that should be controlled)
The purpose of the air conditioning system is to control temperature, the air flow and humidity within the aircraft cabin.
What temperature range is the aircraft cabin maintained to?
21 - 27 degrees
What is the purpose of trim air valves?
How many trim air valves are on an aircraft?
The trim air valves add an adjustable quantity of hot trim air from the engine to the cooled conditioned air from the mixer unit/ pack output
Each zone/pack will have a trim air valve and so the number of trim air valves depends on the number of zones
List the components of a vapour cycle system in order.
(also discription)
- Compressor - Increases temperature and pressure to make system more efficient
- Condensor - Refrigerant heat given up to outside ambient temperature
- Receiver Dryer - Dessicant that absorbs any moisture in the system
- Thermostatic / thermal expansion valve - regulates the amount of refrigerant liquid flowing into the evaporator
- Evaporator - Hot air taken from the cabin and transferred into the refrigerant
Explain the operation of the Vapour Cycle System
The vapor cycle system is an older air conditioning system that used refrigerant as medium to cool aircraft. It was used on older aircraft to cool cockpit and cabin.
The evarporator takes hot air from the cabin and transfers it to the refrigerant, evaporating it in the process.
It then flows to the compressor which heats it further and increases its temperature.
Hot and high pressure refrigerant then flows through the condensor where the heat is transferred to the outside ambient air. Refrigerant condenses.
Then flows through the Reciever Dryer which uses a dessicant to absorb any moisture
Then flows through the thermostatic/thermal expansion valve which only allows a certain amount of refrigerant into the evaporator.
List the components of an air-cycle system? (discription)
Compressor - increases heat and pressure of bleed air
Heat exchanger - heat in air transferred to ambient air
Turbine - takes energy from air cooling it further, uses this energy to drive compressor and cooling fan
Water separator - Absorbs the moisture from the air and re-uses it to make ambient air even colder by injecting it into stream
Pack anti -ice valve - can remove ice using warm air
Turbine bypass valve - controls output temperature along with RAM air inlet door
Flow control valve
How is heat removed in the ACM turbine?
The turbine takes energy from the air, with which the compressor and cooling fan are driven.
Removing energy from the air removes heat from it
'’Removing energy (cooling) atoms and molecules decreases their motion, resulting in a decrease in temperature’’
Heat exchanger also removes heat, but all to a lesser degree than the turbine
How is water removed from the conditioned air?
Water separator - separates, collects and removes excess moisture from the air before it enters the cabin.
It then uses this water to further cool Ram air increasing efficiency
What is the purpose of a pack valve?
Pack valve = Flow Control valve
The Pack valve/ Flow control valve allows a certain amount of bleed air from the engine through to the pack system and as trim air
I.e If one pack system fails, the flow control valve feeding that pack will need to be closed.
What is the purpose of recirculation fans and what percentage of the air is recirculated?
Recirculates air that is already in the cabin which reduces the workload of the packs
30-55% of the air in the cabin is recirculated
Is the isolation valve normally open or closed in normal flight?
The isolation valve is normally closed in flight